US3080912A - Gas burners - Google Patents

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US3080912A
US3080912A US747959A US74795958A US3080912A US 3080912 A US3080912 A US 3080912A US 747959 A US747959 A US 747959A US 74795958 A US74795958 A US 74795958A US 3080912 A US3080912 A US 3080912A
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gas
burner
air
openings
spaced
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US747959A
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William R Winter
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CBS Corp
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Westinghouse Electric Corp
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • F23D14/04—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner
    • F23D14/10—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner with elongated tubular burner head

Definitions

  • This invention relates to gas furnaces such as are used for air heating, and has as an object to improve the gas burners used in 'such' furnaces.
  • a feature of this invention is that it provides a slotted gas burner which is compact, which has a low manufacturing cost, which produces with a high air-to-gas ratio, the short flame characteristic desired in the tubular heat exchangers, which burns all available gases, and which is quiet in operation from ignition to extinction.
  • FIG. 1 is an enlarged plan view of one of a gas burner embodying this invention
  • FIG. 2 is an end view looking at the left end of FIG. 1;
  • FIG. 3 is a section along the line 33 of FIG. 1, showing in addition, the lower ends of heat exchange tubes of an associated furnace aligned with the ports of the gas burner;
  • FIG. 4 is an enlarged fragmentary view of the baffle of FIGS. 1, 2, and 3;
  • FIG. 5 is a section along the line 55 of FIG. 3;
  • FIG. 6 is a section along the line 6-6 of FIG. 3;
  • FIG. 7 is a section along the line 77 of FIG. 3;
  • FIG. 8 is a section along the line 8-8 of FIG. 3;
  • FIG. 9 is a fragmentary section along the line 99 of FIG. 3;
  • FIG. 10 is a fragmentary section along the line 10-10 of FIG. 1, and
  • FIG. 11 is a fragmentary section along the line 1111 of FIG. 3.
  • a gas burner 35 has six, spaced-apart, distributed burner ports 50 aligned with the lower ends of corresponding heat exchange tubes 30 of a furnace which is not shown. Each burner 35 has a primary air inlet 38 connecting with a converging air passage 37 within which is supported by clamps 60, a gas supply tube 36.
  • Each burner 35 has inwardly of the gas tube 36, an air-gas passage 46 shaped as a venturi, of which the passage 37 is the entrance, and which supplies the mixture of primary air and gas into a baffle assembly 49.
  • Each burner 35 has between the ends of its passage 46, a lower portion curved in a circular arc with a stiffening flange 47 at its bottom center, and opposite its flange 47 has side walls 48 which are spaced apart and which support therebetween the bafile assembly 49. Beyond the outer end of its passage '46, each burner 35 has, as shown by FIG. 8, only the baffle supporting side walls 48 and the flange 47.
  • each burner 35 where they join its curved portion are pinched together as shown by FIGS. 1, 3 and 5 from the outer end of the passage 46, the end closest the air inlet 38, to close off the air-gas passage 46 to prevent it from discharging directly into the baffle assembly opposite the adjacent tubes 30 closest to air and gas inlets.
  • the walls 48 where they join the rounded head portion are spaced apart to form a gradually diverging passage 60 through which the passage 46 can discharge into the baffle assembly 49.
  • the walls 48 are uniformly spaced apart to provide a wider passage 51 to the baflle assembly 49.
  • passages between the 3,080,912 Patented Mar. 12, 1963 passage 46 and the baflle assembly 49 are shaped as described to prevent the tube 30 nearest the air and gas inlet end of the passage 36 from being over-supplied, and the other-tubes under-supplied with the air-gas mixture.
  • Each baffle assembly 49 consists of four, spaced-apart, parallel, metal sheets 55, 56, 57 and 58 arranged in the order named,from the top to the bottom of the baflle assembly, the top sheet 55 being nearest to and extending parallel to the aligned, open ends of the assembled tubes 30, and the bottom sheet 58 being nearest the air-gas passage 46.
  • the top sheet 55 and the two intermediate sheets 56 and 57 have circular openings 50 aligned with the ends of the corresponding tubes 30, the openings 50 in the top sheet forming the previously mentioned distributes burner ports.
  • the intermediate sheets 56 and 57 also have aligned circular openings 61 halfway between adjacent pairs of openings 50.
  • the bottom sheet 58 has circular openings 62 aligned with openings 61.
  • the primary air-gas supplied to a battle assembly enters the openings 62 in a lower sheet 58, and then splits into streams between the sheets 58 and 57, passes through openings 50 and 61 in the sheet 57, splits into streams between the sheets 57 and 56, passes through openings 50 and 61 in the sheet 56, splits into streams between the sheets 56 and 55, and finally passes out the openings 50 in the sheet 55, into the lower ends of the associated tubes 30.
  • the lower ends of the tubes 30 are spaced from the top sheet 55 as shown by FIG. 3, and secondary air enters the lower ends of the tubes 30, 360 around the aligned batfle openings 50.
  • the baffle assembly is provided with the tortuous airgas passages for preventing flash-back which is successfully prevented despite the relatively large volume of primary air supplied into the venturi 46. In prior arrangements, such large volumes of primary air often resulted in undesired flash-back.
  • the burner side walls 48 are formed along their upper edges as corrugated ribbons, having corrugated portions spaced outwardly from each side of the baifle assembly as shown in FIGS. 911, and between the dimpled portions 70 contacting and supporting the sides of the baflie assembly as shown by FIGS. 5-7.
  • the corrugated portions 70 provide closely spaced ports for transmitting a flame from an end port that is lighted first to the other ports.
  • each baflle assembly has a pair of corrugated portions 64 at each of its ends, forming airgas passages 71 which are directed towards correspondingly formed air-gas passages 71 of adjacent sheets 55 of adjacent burners, and serve to transmit flame from the first lighted burner to the burners on each side of it.
  • a pilot burner which is not shown establishes a flame in the open end of an end tube 30.
  • the flame propogates through ports formed by corrugated portions 70 to the remainder of the tubes 30.
  • the flame from the row of tubes 30 is propogated through the passages 71 of the end sheet 55 of that row to an adjacent row of tubes which is not shown.
  • a gas burner having a curved lower portion with an air and gas inlet opening in one end, having spacedapart, upwardly extending sides joining with said curved portion, and a baflle assembly supported between the upper portions of said sides, said assembly including a top sheet having a plurality of ports extending along its longitudinal center and spaced too far apart to permit chain ignition, one from another, including a bottom sheet having spaced-apart openings for the admission of mixed air and gas, and including baffle mean-s between said sheets for extending the lengths of the paths of the mixed air and gas passing between said openings and said ports, said sides having upper portions which contact the sides of said assembly at a plurality of spacedapart points which are substantially closer spaced than are said parts, and between said points are spaced from said sides of said assembly to form mixed air and gas openings substantially larger in number, smaller in size, and more closely spaced than said ports, by means of which a flame at an end one of said ports can be propagated by said last mentioned openings alongside said top sheet.
  • a gas burner as claimed in claim 1 in which said top sheet has outwardly extending portions at its ends with upwardly extending bulges therein, and in which the tops of said sides of said burner at their ends extend outwardly under said bulges for forming with said bulges, transverse passages for transmitting flames to similarly formed passages of adjacent similar burners.
  • a gas burner as claimed in claim 1 in which the spacing between the lower portions of said sides of said burned is tapered from no spacing opposite the one of said ports closest to said inlet opening to maximum spacing opposite the one of said ports most remote from said inlet opening.
  • a gas burner as claimed in claim 1 in which the lower portions of said sides of said burner adjacent to where they join said curved portion are pinched together to close off the passage between said sides of said burner opposite the one of said ports nearest said inlet opening, and between said one port and others of said ports, said sides of said burner are progressively separated to form a wider passage therebetween opposite said other ports.
  • a gas burner as claimed in claim 4 in which said top sheet has outwardly extending portions at its ends with upwardly extending bulges therein, and in which the tops of said sides of said burner at their ends outwardly under said bulges for forming with said bulges, transverse passages for transmitting flames to similarly formed passages of adjacent similar burners.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)

Description

March 12, 1963 w. R. WINTER GAS BURNERS 2 Sheets-Sheet 1 Filed July 11, 1958 March 12, 1963 w. R. WINTER GAS BURNERS 2 Sheets-Sheet 2 Filed July 11, 1958 United States Patent 3,080,912 GAS BURNERS William R. Winter, Staunton, Va., assignor to Westinghouse Electric Corporation, East Pittsburgh, Pa., a corporation of Pennsylvania Filed July 11, 1958, Ser. No. 747,959 Claims. (Cl. 158114) This invention relates to gas furnaces such as are used for air heating, and has as an object to improve the gas burners used in 'such' furnaces.
A feature of this invention is that it provides a slotted gas burner which is compact, which has a low manufacturing cost, which produces with a high air-to-gas ratio, the short flame characteristic desired in the tubular heat exchangers, which burns all available gases, and which is quiet in operation from ignition to extinction.
This invention will now be described with reference to the annexed drawings, of which:
FIG. 1 is an enlarged plan view of one of a gas burner embodying this invention;
FIG. 2 is an end view looking at the left end of FIG. 1;
FIG. 3 is a section along the line 33 of FIG. 1, showing in addition, the lower ends of heat exchange tubes of an associated furnace aligned with the ports of the gas burner;
FIG. 4 is an enlarged fragmentary view of the baffle of FIGS. 1, 2, and 3;
FIG. 5 is a section along the line 55 of FIG. 3;
FIG. 6 is a section along the line 6-6 of FIG. 3;
FIG. 7 is a section along the line 77 of FIG. 3;
FIG. 8 is a section along the line 8-8 of FIG. 3;
FIG. 9 is a fragmentary section along the line 99 of FIG. 3;
FIG. 10 is a fragmentary section along the line 10-10 of FIG. 1, and
FIG. 11 is a fragmentary section along the line 1111 of FIG. 3.
A gas burner 35 has six, spaced-apart, distributed burner ports 50 aligned with the lower ends of corresponding heat exchange tubes 30 of a furnace which is not shown. Each burner 35 has a primary air inlet 38 connecting with a converging air passage 37 within which is supported by clamps 60, a gas supply tube 36.
Each burner 35 has inwardly of the gas tube 36, an air-gas passage 46 shaped as a venturi, of which the passage 37 is the entrance, and which supplies the mixture of primary air and gas into a baffle assembly 49. Each burner 35 has between the ends of its passage 46, a lower portion curved in a circular arc with a stiffening flange 47 at its bottom center, and opposite its flange 47 has side walls 48 which are spaced apart and which support therebetween the bafile assembly 49. Beyond the outer end of its passage '46, each burner 35 has, as shown by FIG. 8, only the baffle supporting side walls 48 and the flange 47.
The side walls 48 of each burner 35 where they join its curved portion are pinched together as shown by FIGS. 1, 3 and 5 from the outer end of the passage 46, the end closest the air inlet 38, to close off the air-gas passage 46 to prevent it from discharging directly into the baffle assembly opposite the adjacent tubes 30 closest to air and gas inlets. From just beyond the center of the second tube 30 from the air-gas inlet end of the burner, the walls 48 where they join the rounded head portion are spaced apart to form a gradually diverging passage 60 through which the passage 46 can discharge into the baffle assembly 49. Opposite the fourth, fifth and sixth tubes 30 from the inlet end of the passage 36, the walls 48 are uniformly spaced apart to provide a wider passage 51 to the baflle assembly 49. The passages between the 3,080,912 Patented Mar. 12, 1963 passage 46 and the baflle assembly 49 are shaped as described to prevent the tube 30 nearest the air and gas inlet end of the passage 36 from being over-supplied, and the other-tubes under-supplied with the air-gas mixture.
Each baffle assembly 49 consists of four, spaced-apart, parallel, metal sheets 55, 56, 57 and 58 arranged in the order named,from the top to the bottom of the baflle assembly, the top sheet 55 being nearest to and extending parallel to the aligned, open ends of the assembled tubes 30, and the bottom sheet 58 being nearest the air-gas passage 46. The top sheet 55 and the two intermediate sheets 56 and 57 have circular openings 50 aligned with the ends of the corresponding tubes 30, the openings 50 in the top sheet forming the previously mentioned distributes burner ports. The intermediate sheets 56 and 57 also have aligned circular openings 61 halfway between adjacent pairs of openings 50. The bottom sheet 58 has circular openings 62 aligned with openings 61.
The primary air-gas supplied to a battle assembly enters the openings 62 in a lower sheet 58, and then splits into streams between the sheets 58 and 57, passes through openings 50 and 61 in the sheet 57, splits into streams between the sheets 57 and 56, passes through openings 50 and 61 in the sheet 56, splits into streams between the sheets 56 and 55, and finally passes out the openings 50 in the sheet 55, into the lower ends of the associated tubes 30. The lower ends of the tubes 30 are spaced from the top sheet 55 as shown by FIG. 3, and secondary air enters the lower ends of the tubes 30, 360 around the aligned batfle openings 50.
The baffle assembly is provided with the tortuous airgas passages for preventing flash-back which is successfully prevented despite the relatively large volume of primary air supplied into the venturi 46. In prior arrangements, such large volumes of primary air often resulted in undesired flash-back.
The burner side walls 48 are formed along their upper edges as corrugated ribbons, having corrugated portions spaced outwardly from each side of the baifle assembly as shown in FIGS. 911, and between the dimpled portions 70 contacting and supporting the sides of the baflie assembly as shown by FIGS. 5-7. The corrugated portions 70 provide closely spaced ports for transmitting a flame from an end port that is lighted first to the other ports.
The top sheet 55 of each baflle assembly has a pair of corrugated portions 64 at each of its ends, forming airgas passages 71 which are directed towards correspondingly formed air-gas passages 71 of adjacent sheets 55 of adjacent burners, and serve to transmit flame from the first lighted burner to the burners on each side of it.
A pilot burner which is not shown establishes a flame in the open end of an end tube 30. The flame propogates through ports formed by corrugated portions 70 to the remainder of the tubes 30. The flame from the row of tubes 30 is propogated through the passages 71 of the end sheet 55 of that row to an adjacent row of tubes which is not shown.
I claim:
1. A gas burner having a curved lower portion with an air and gas inlet opening in one end, having spacedapart, upwardly extending sides joining with said curved portion, and a baflle assembly supported between the upper portions of said sides, said assembly including a top sheet having a plurality of ports extending along its longitudinal center and spaced too far apart to permit chain ignition, one from another, including a bottom sheet having spaced-apart openings for the admission of mixed air and gas, and including baffle mean-s between said sheets for extending the lengths of the paths of the mixed air and gas passing between said openings and said ports, said sides having upper portions which contact the sides of said assembly at a plurality of spacedapart points which are substantially closer spaced than are said parts, and between said points are spaced from said sides of said assembly to form mixed air and gas openings substantially larger in number, smaller in size, and more closely spaced than said ports, by means of which a flame at an end one of said ports can be propagated by said last mentioned openings alongside said top sheet.
2. A gas burner as claimed in claim 1 in which said top sheet has outwardly extending portions at its ends with upwardly extending bulges therein, and in which the tops of said sides of said burner at their ends extend outwardly under said bulges for forming with said bulges, transverse passages for transmitting flames to similarly formed passages of adjacent similar burners.
3. A gas burner as claimed in claim 1 in which the spacing between the lower portions of said sides of said burned is tapered from no spacing opposite the one of said ports closest to said inlet opening to maximum spacing opposite the one of said ports most remote from said inlet opening.
4. A gas burner as claimed in claim 1 in which the lower portions of said sides of said burner adjacent to where they join said curved portion are pinched together to close off the passage between said sides of said burner opposite the one of said ports nearest said inlet opening, and between said one port and others of said ports, said sides of said burner are progressively separated to form a wider passage therebetween opposite said other ports.
5. A gas burner as claimed in claim 4 in which said top sheet has outwardly extending portions at its ends with upwardly extending bulges therein, and in which the tops of said sides of said burner at their ends outwardly under said bulges for forming with said bulges, transverse passages for transmitting flames to similarly formed passages of adjacent similar burners.
References Cited in the file of this patent UNITED STATES PATENTS 2,194,733 Anderson et al Mar. 26, 1940 2,255,636 Wittmann Sept. 9, 1941 2,289,759 Denise July 14, 1942 2,465,151 Dresen Mar. 22, 1949 2,499,482 Flynn Mar. 7, 1950 2,572,273 Miller et al Oct. 23, 1951 2,670,790 Marble Mar. 2, 1954 2,875,821 Allen Mar. 3, 1959 FOREIGN PATENTS 328,738 France Jan. 23, 1903 853,952 Germany Oct. 30, 1952 685,855 Great Britain Jan. 14, 1953 1,127,936 France Aug. 20, 1956

Claims (1)

1. A GAS BURNER HAVING A CURVED LOWER PORTION WITH AN AIR AND GAS INLET OPENING IN ONE END, HAVING SPACEDAPART, UPWARDLY EXTENDING SIDES JOINING WITH SAID CURVED PORTION, AND A BAFFLE ASSEMBLY SUPPORTED BETWEEN THE UPPER PORTIONS OF SAID SIDES, SAID ASSEMBLY INCLUDING A TOP SHEET HAVING A PLURALITY OF PORTS EXTENDING ALONG ITS LONGITUDINAL CENTER AND SPACED TOO FAR APART TO PERMIT CHAIN IGNITION, ONE FROM ANOTHER, INCLUDING A BOTTOM SHEET HAVING SPACED-APART OPENINGS FOR THE ADMISSION OF MIXED AIR AND GAS, AND INCLUDING BAFFLE MEANS BETWEEN SAID SHEETS FOR EXTENDING THE LENGTHS OF THE PATHS OF THE MIXED AIR AND GAS PASSING BETWEEN SAID OPENINGS AND
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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3132642A (en) * 1962-07-23 1964-05-12 John A Fingland Pavement burner
US3351048A (en) * 1964-09-11 1967-11-07 Fostoria Fannon Inc Infra-red gas burner structure
JPS5043231Y1 (en) * 1970-12-25 1975-12-10
US5062788A (en) * 1989-01-10 1991-11-05 Haden-Schweitzer Corporation High efficiency linear gas burner assembly
US20040250810A1 (en) * 2003-06-12 2004-12-16 Honeywell International Inc. Warm air furnace with premix burner
US20040253559A1 (en) * 2003-06-12 2004-12-16 Honeywell International Inc. Premix burner for warm air furnace
US20130213378A1 (en) * 2012-02-17 2013-08-22 Honeywell International Inc. Burner system for a furnace
US8919337B2 (en) 2012-02-17 2014-12-30 Honeywell International Inc. Furnace premix burner
US9605871B2 (en) 2012-02-17 2017-03-28 Honeywell International Inc. Furnace burner radiation shield

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR328738A (en) * 1903-01-23 1903-07-18 Georges Ymonet Gas heater with uniform pressure and flow
US2194733A (en) * 1937-09-08 1940-03-26 Pennsylvania Furnace & Iron Co Air heating furnace
US2255636A (en) * 1939-09-16 1941-09-09 Chicago By Products Corp Gas burner
US2289759A (en) * 1940-10-22 1942-07-14 Gen Properties Company Inc Warm air heater
US2465151A (en) * 1945-09-27 1949-03-22 Rocky Mountain Gas Equipment C Furnace with thermostatic control of convection mediums
US2499482A (en) * 1947-12-18 1950-03-07 John H Flynn Ribbon-type gas burner
US2572273A (en) * 1946-12-31 1951-10-23 Mission Appliance Corp Sheet metal gas burner with internal fuel distributor
DE853952C (en) * 1951-02-11 1952-10-30 Benno Schilde Maschb Ag Gas heated air heater
GB685855A (en) * 1950-03-02 1953-01-14 Turley & Williams Ltd Improvements in and connected with gas burners
US2670790A (en) * 1949-11-07 1954-03-02 Internat Sales Company Sheet metal fuel gas burner construction
FR1127936A (en) * 1955-06-13 1956-12-27 Infrared radiant panel
US2875821A (en) * 1954-11-09 1959-03-03 Stewart Warner Corp Sheet metal burner and cross lighter

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR328738A (en) * 1903-01-23 1903-07-18 Georges Ymonet Gas heater with uniform pressure and flow
US2194733A (en) * 1937-09-08 1940-03-26 Pennsylvania Furnace & Iron Co Air heating furnace
US2255636A (en) * 1939-09-16 1941-09-09 Chicago By Products Corp Gas burner
US2289759A (en) * 1940-10-22 1942-07-14 Gen Properties Company Inc Warm air heater
US2465151A (en) * 1945-09-27 1949-03-22 Rocky Mountain Gas Equipment C Furnace with thermostatic control of convection mediums
US2572273A (en) * 1946-12-31 1951-10-23 Mission Appliance Corp Sheet metal gas burner with internal fuel distributor
US2499482A (en) * 1947-12-18 1950-03-07 John H Flynn Ribbon-type gas burner
US2670790A (en) * 1949-11-07 1954-03-02 Internat Sales Company Sheet metal fuel gas burner construction
GB685855A (en) * 1950-03-02 1953-01-14 Turley & Williams Ltd Improvements in and connected with gas burners
DE853952C (en) * 1951-02-11 1952-10-30 Benno Schilde Maschb Ag Gas heated air heater
US2875821A (en) * 1954-11-09 1959-03-03 Stewart Warner Corp Sheet metal burner and cross lighter
FR1127936A (en) * 1955-06-13 1956-12-27 Infrared radiant panel

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3132642A (en) * 1962-07-23 1964-05-12 John A Fingland Pavement burner
US3351048A (en) * 1964-09-11 1967-11-07 Fostoria Fannon Inc Infra-red gas burner structure
JPS5043231Y1 (en) * 1970-12-25 1975-12-10
US5062788A (en) * 1989-01-10 1991-11-05 Haden-Schweitzer Corporation High efficiency linear gas burner assembly
US20040250810A1 (en) * 2003-06-12 2004-12-16 Honeywell International Inc. Warm air furnace with premix burner
US20040253559A1 (en) * 2003-06-12 2004-12-16 Honeywell International Inc. Premix burner for warm air furnace
US6880548B2 (en) 2003-06-12 2005-04-19 Honeywell International Inc. Warm air furnace with premix burner
US6923643B2 (en) * 2003-06-12 2005-08-02 Honeywell International Inc. Premix burner for warm air furnace
US20130213378A1 (en) * 2012-02-17 2013-08-22 Honeywell International Inc. Burner system for a furnace
US8919337B2 (en) 2012-02-17 2014-12-30 Honeywell International Inc. Furnace premix burner
US9605871B2 (en) 2012-02-17 2017-03-28 Honeywell International Inc. Furnace burner radiation shield

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